Spacecraft Equipped with a Space Debris Removal System (Aerothermodynamics, Bulk–Mass Characteristics and Trajectories of Spacecraft Descent from Near-Earth Orbits) von Finchenko, V. S., Ivankov, A. A., Shmatov, S. I.

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Study of defects of elastic thermal protection by inverse methods of nonlinear acoustics von Nenarokomov, A V, Alifanov, O M, Nenarokomov, K A, Titov, D M, Finchenko, V S

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Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project von Golomazov, M. M., Finchenko, V. S.

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Proposal for Creating a Device for Deorbiting Low-Earth-Orbit CubeSats von Nesterin, I. M., Pichhadze, K. M., Sysoev, V. K., Finchenko, V. S., Firsyuk, S. O., Yudin, A. D.

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Transformable descent vehicles von Pichkhadze, K. M., Finchenko, V. S., Aleksashkin, S. N., Ostreshko, B. A.

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Thermal destruction calculation method and its results for Fregat Versatile Space Tug during entry into the Earth’s atmosphere von Finchenko, V. S., Ustinov, S. N., Ivankov, A. A.

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Preliminary results of the calculated and experimental studies of the basic aerothermodynamic parameters of the ExoMars landing module von Finchenko, V. S., Ivankov, A. A., Shmatov, S. I., Mordvinkin, A. S.

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A method of rapidly calculating how a rarefied atmosphere acts on a spacecraft von Finchenko, V. S., Shmatov, S. I.

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The Numerical Simulation of Aerodynamics of the Frontal Aerodynamic Screen of ExoMars Project Descent Vehicle and the Analysis of Flow Pattern in the Base Area and Near Wake von Babakov, A. V., Finchenko, V. S.

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Design principles of descent vehicles with an inflatable braking device von Alexashkin, S. N., Pichkhadze, K. M., Finchenko, V. S.

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Method for the Preliminary Thermal Analysis of the Dashboard of the Lunar Lander: Part 1. Rapid Thermal Analysis of the Dashboard von Bugrova, A. D., Kotlyarov, E. Yu, Finchenko, V. S.

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Method for the Preliminary Thermal Analysis of the Dashboard of the Lunar Lander: Part 2. Measurement of the Temperature of Mounting Seats and TCS Modification Options von Bugrova, A. D., Kotlyarov, E. Yu, Finchenko, V. S.

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Theoretical and Experimental Study of Subsonic Gas Flow Around the Frontal Aerodynamic Screen After Separation from the ExoMars Vehicle Descending in the Atmosphere of the Planet von Babakov, A. V., Finchenko, V. S.

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Program package for the computer-aided aerodynamic design system for descent vehicles in planetary atmospheres von Golomazov, M. M., Finchenko, V. S., Ivankov, A. A., Shmatov, S. I.

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Results of integrated development tests of the Phobos-Grunt spacecraft’s descent module intended to deliver Phobos soil samples to Earth von Alexashkin, S. N., Martynov, M. B., Pichkhadze, K. M., Finchenko, V. S.

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Numerical study of thermal destruction of the "Chelyabinsk" meteorite when entering the Earths atmosphere von Finchenko, V. S., Ivankov, A. A.

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On the Use of Inflatable Decelerators in the Design of Spacecraft Intended for the Study of Venus von Finchenko, V. S., Ivankov, A. A., Golomazov, M. M., Shmatov, S. I.

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Aerothermodynamics calculation of thermal destruction of “Fregat” upper stage at descent in the Earth's atmosphere von Glazunov, A. A., Goldin, V. D., Zverev, V. G., Ustinov, S. N., Finchenko, V. S.

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Supersonic flow around a body of small elongation von Guvernyuk, S. V., Zubkov, A. F., Pichkhadze, K. M., Finchenko, V. S., Shvets, A. I.

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Calculation of Radiation Heat Transfer in Problems of Flow past Bodies with Account for Heat-Shield Coating Mass Loss von Borisov, V. M., Golomazov, M. M., Ivankov, A. A., Finchenko, V. S.

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